- Effective
- May 31, 2016
- Published
- May 11, 2016 · 81 FR 29125–29127
- Issued
- May 4, 2016
- Model
- DHC-3
- Data sheet
- TCDSA-815
- Registered aircraft
- 76 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-18514
- Docket
- FAA-2016-6628
- Project
- 2016-CE-013-AD
- Issued as
- Final rule; request for comments
Unofficial copy from the Federal Register XML, document 2016-10928. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| Official PDF | 234 KB | c5c555be…08e1eaf | 2016-10928.pdf on govinfo.gov |
| Official PDF | 207 KB | 44780af8…0e17a36 | 2016-12468.pdf on govinfo.gov |
| Federal Register XML | 20 KB | 9a3fb8e0…d038617 | 2016-10928.xml on federalregister.gov |
| Federal Register XML | 12 KB | bc009a10…cc1f708 | 2016-12468.xml on federalregister.gov |
| FAA DRS HTML attachment | 61 KB | 8be8b26a…2872f10 | FAA DRS (API key needed) |
| FAA DRS PDF attachment | 59 KB | c6b586d7…5310fba | FAA DRS (API key needed) |
| FAA DRS PDF | 44 KB | 083a909c…e2aefd2 | FAA DRS (API key needed) |
On this page
Summary
The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to Viking Air Limited Model DHC-3 airplanes that are modified with the Baron Short Take Off and Landing (STOL) kit (Supplemental Type Certificate SA94-114 or SA 00287NY). The Code of Federal Regulations reference for records maintenance cited in last sentence in paragraph (f) is incorrect. This document corrects that error. In all other respects, the original document remains the same; however we are publishing the entire rule in the Federal Register.
The airworthiness directive
2016-10-03 Viking Air Limited: Amendment 39-18514; Docket No. FAA-2016-6628; Directorate Identifier 2016-CE-013-AD.
(a) Effective Date
PDF page 2This airworthiness directive (AD) becomes effective May 31, 2016.
(b) Affected ADs
PDF page 2None.
(c) Applicability
PDF page 2This AD applies to Viking Air Limited Model DHC-3 airplanes, all serial numbers, that are:
(1) Modified with the Baron Short Take Off and Landing (STOL) kit (Supplemental Type Certificate SA94-114 or SA 00287NY); and
(2) certificated in any category.
(d) Subject
PDF page 2Air Transport Association of America (ATA) Code 8: Leveling and Weighing.
(e) Reason
PDF page 2This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as an accident report that indicated that the center of gravity was too far aft and contributed to a stall during takeoff. We are issuing this AD to correct the center of gravity and prevent such a stall during takeoff and loss of control during other phases of flight.
(f) Actions and Compliance
PDF page 2Unless already done, within 30 days after May 31, 2016 (the effective date of this AD), remove whichever previous revision of the Otter Baron short take-off and landing (STOL) kit installation flight manual supplement (FMS) that is currently being used and incorporate Stolairus Aviation Inc. Flight Manual Supplement #4 for de Havilland DHC-3 Otter with the Baron STOL Kit Installation, Revision 3, dated May 22, 2015. This action may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the aircraft records showing compliance with this AD in accordance with 14 CFR 43.9(a)(1)-(4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417, 121.380, or 135.439.
(g) Other FAA AD Provisions
PDF page 2The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Aziz Ahmed, Aerospace Engineer, FAA, New York Aircraft Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone: (516) 287-7329; fax: (516) 794-5531; email: aziz.ahmed@faa.gov. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.
(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service.
(h) Related Information
PDF page 2Refer to MCAI Transport Canada AD CF-2016-05, dated January 25, 2016, for related information. You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-6628.
(i) Material Incorporated by Reference
PDF page 2(1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Stolairus Aviation Inc., Flight Manual Supplement #4, de Havilland DHC-3 Otter, Baron STOL Kit Installation, DOT STC # SA 94-114/FAA STC # SA 00287 NY, Revision 3, dated May 22, 2015.
(ii) Reserved.
(3) For Stolairus Aviation Inc. service information identified in this AD, contact Stolairus Aviation Inc. (formerly known as AOG Air Support, Inc.), 6095 Airport Way, Kelowna, British Columbia V1V 1S1; phone: (250) 491-7511; fax: (25) 491-7522; Internet: http://www.stolairus.com.
(4) You may view this service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. It is also available on the Internet at http://www.regulations.gov by searching for locating Docket No. FAA-2016-6628.
(5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
DatesPage 1
This final rule is effective May 31, 2016.
AddressesPage 1
You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-6628; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: 800-647-5527) is Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
For further information contactPage 1
Aziz Ahmed, Aerospace Engineer, FAA, New York Aircraft Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone: (516) 287-7329; fax: (516) 794-5531; email: aziz.ahmed@faa.gov.
Supplementary informationPage 2
Airworthiness Directive 2016-10-03, Amendment 39-18514 (81 FR 29125, May 11, 2016), requires removing whichever previous revision of the Otter Baron short take-off and landing (STOL) kit installation flight manual supplement (FMS) that is currently being used and incorporate Stolairus Aviation Inc. Flight Manual Supplement #4 for de Havilland DHC-3 Otter with the Baron STOL Kit Installation, Revision 3, dated May 22, 2015, for Viking Air Limited Model DHC-3 airplanes that are modified with the Baron Short Take Off and Landing (STOL) kit (Supplemental Type Certificate SA94-114 or SA 00287NY).
As published, the Code of Federal Regulations (CFR) reference for records maintenance cited in the last sentence in paragraph (f) is incorrect. The published reference is 14 CFR 91.173 or 135.439, and it is should be 14 CFR 91.417, 121.380, or 135.439.
Although no other part of the preamble or regulatory information has been corrected, we are publishing the entire rule in the Federal Register.
Adoption of the amendmentPage 2
The effective date of this AD remains May 31, 2016.
1. The authority citation for part 39 continues to read as follows:
2. The FAA amends § 39.13 by adding the following new AD:
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 76
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1953 | 6 |
|---|---|
| 1954 | 6 |
| 1955 | 4 |
| 1956 | 10 |
| 1957 | 4 |
| 1958 | 10 |
| 1959 | 1 |
| 1960 | 7 |
| 1961 | 6 |
| 1962 | 2 |
| 1965 | 2 |
| 1966 | 1 |
17 with no year recorded